Traveling-wave tube amplifiers for high-frequency signals, including terahertz signals, and methods for making a slow-wave structure for the traveling-wave tube amplifiers are provided. The slow-wave structures include helical conductors that are self-assembled via the release and relaxation of strained films from a sacrificial growth substrate.
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1. A traveling wave tube amplifier comprising:
a slow-wave structure comprising:
a cylindrical scaffold comprising a dielectric film, the cylindrical scaffold having an interior surface; and
an electrically conductive helix on the interior surface of the cylindrical scaffold, the electrically conductive helix comprising a plurality of electrically conductive strips connected end-to-end;
an electron gun positioned to direct one or more beams of electrons axially through the electrically conductive helix or around the periphery of the electrically conductive helix; and
an electron collector positioned opposite the electron gun.
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This invention was made with government support under DE-FG02-03ER46028 awarded by the US Department of Energy and under FA9550-19-1-0086 awarded by the USAF/AFOSR. The government has certain rights in the invention.
A traveling wave tube (TWT) is a beam-wave structure enabling interaction between an energetic beam of electrons and an electromagnetic (EM) wave to transfer energy from the electron beam to the EM wave for amplification. TWTs are used as compact, high-gain, high-power sources of high-frequency radiation in applications such as wireless communications, biomedical imaging, and radar. Central to the amplification process is a slow-wave structure (SWS) that matches the phase velocity of the EM wave to that of the electron beam; this structure is some form of meander transmission line or, more commonly, a conductive helix. The slow-wave structure conducts the traveling EM wave along a pathway whose total length is greater than the axial dimension along which the electron beam travels; thus, the component of the EM wave velocity along the axial dimension matches that of the electron beam.
Conventional TWT structures use a wire helix whose dimensions are limited by the smallest gauge wire available, the ability to wind the helix with precision, the ability to support the helix to keep it aligned with the electron beam, and the ability to handle and assemble the helix into the structure. Other methods for manufacturing helical SWSs rely on high-precision laser manufacturing and wafer bonding. Unfortunately, these methods are not easily scalable to micro-scale dimensions (and thus higher frequencies) and are not mass-producible on inexpensive and large-area substrates.
TWT amplifiers and methods for making SWSs for TWT amplifiers are provided.
One embodiment of a traveling wave tube amplifier includes a slow-wave structure that includes: a cylindrical scaffold comprising a dielectric film, the cylindrical scaffold having an interior surface; and an electrically conductive helix on the interior surface of the cylindrical scaffold, the electrically conductive helix comprising a plurality of electrically conductive strips connected end-to-end; an electron gun positioned to direct one or more beams of electrons axially through the electrically conductive helix or around the periphery of the electrically conductive helix; and an electron collector positioned opposite the electron beam source.
One embodiment of a method of making a slow-wave structure includes the steps of: forming a dielectric support membrane on a device substrate; forming a sacrificial film on a portion of a surface of the dielectric support membrane; forming a scaffold film comprising a strained dielectric material on a portion of a surface of the sacrificial film; forming a plurality of parallel, electrically conductive strips on the scaffold film, each of the electrically conductive strips having a leading end and a trailing end, wherein an edge of the scaffold film or the trailing ends of the electrically conductive strips are attached to the dielectric support membrane; selectively removing the sacrificial film underlying the scaffold film, wherein the scaffold film relaxes and rolls into a cylinder, bringing the electrically conducting strips into an end-to-end arrangement that forms a helix on an interior surface of the cylinder; electroplating the surface of the helix with an electrically conductive material; forming a first electrically conductive contact in electrical communication with a first end of the helix; and forming a second electrically conductive contact in electrical communication with the second end of the helix.
Other principal features and advantages of the invention will become apparent to those skilled in the art upon review of the following drawings, the detailed description, and the appended claims.
Illustrative embodiments of the invention will hereafter be described with reference to the accompanying drawings, wherein like numerals denote like elements.
TWT amplifiers and methods for making SWSs for TWT amplifiers are provided. The SWSs include helical conductors that are self-assembled via the release and relaxation of strained films from a sacrificial growth substrate. The self-assembly methods enable wafer-level fabrication of SWSs having very small diameters, including micron-scale diameters that enable the amplification of terahertz signals.
The basic components of one embodiment of a TWT amplifier are shown in
When electron beam 104 is emitted from electron gun 102 and accelerated toward electron collector 122, the electrons are in close proximity to the propagating EM wave. The electron beam is directed along the axis of the helix either through the center of the helix or outside of the helix. In some embodiments, multiple electron beams (“beamlets”) are used. These beamlets are directed in circular pattern around the periphery of the helix. The conductive helix slows the axial phase velocity of the EM wave to, or below, the speed of the electrons in the beam. The kinetic energy in the electron beam is coupled into the EM wave, thereby amplifying the EM wave.
Next, a support membrane 204 is formed on at least a portion of the surface of device substrate 202 (
The support membrane is desirably thermally conductive in order to facilitate the dissipation of heat generated by the SWS. However, the requirement for thermal conductivity will depend, at least in part, on the power output of the TWT; a lower power output will generally require a lower thermal conductivity. Diamond and silicon nitride (Si3N4) are examples of low-loss materials that can be used for the support membrane. Because diamond has a higher thermal conductivity, diamond may be a better choice for high-power applications.
A layer of sacrificial material, referred to herein as a sacrificial film 206, is then formed over at least a portion of the surface of support membrane 204 (
Scaffold film 208 is characterized by a film length 210 between a leading edge 211 and a trailing edge 212. Film length 210 is chosen such that, upon release from sacrificial film 206, scaffold film 208 relaxes and rolls into a cylindrical tube with leading edge 211 abutting trailing edge 212. However, leading edge 211 need not come into perfect abutment with trailing edge 212; a small amount of edge overlap or a small gap between the leading and trailing edges is permissible. Film length 210 will depend upon the desired diameter of the SWS. The thickness and strain in scaffold film 208 can be tailored to provide the desired SWS diameter for a targeted frequency. By way of illustration only, a diamond scaffold film having a thickness in the range from about 10 nm to about 20 nm grown on a germanium or photoresist sacrificial layer could provide a tube having an inside diameter in the range from about 0.5 μm to about 2 μm. By way of further illustration, a silicon nitride scaffold film having a thickness in the range from about 20 nm to about 40 nm grown on a germanium sacrificial layer could provide a tube having an inside diameter in the range from about 1 μm to about 5 μm and a silicon nitride scaffold film having a thickness of about 250 nm grown on a germanium sacrificial layer could provide a tube having an inside diameter of about 30 μm.
A plurality of parallel electrically conductive strips 214 is then formed on scaffold film 208 (
Electrically conductive strips 214 should be thin enough that electrically conductive strips 214 do not interfere with the rolling of scaffold film 208 upon the release of scaffold film 208 from sacrificial film 206. By way of illustration, electrically conducting strips 214 will typically have thicknesses in the range from 2 nm to 50 nm. The width and pitch of the strips can be selected to provide a helix with the desired EM wave propagating properties. Both the thickness and the width of the strips can be increased by electroplating after the self-assembly of the cylindrical tube.
Electrically conductive contacts 213, 215 can be deposited when electrically conductive strips 214 are deposited. Alternatively, electrically conductive contacts 213, 215 can be formed at an earlier or later stage of the process. Electrically conductive contacts 213, 215 may be composed of the same material as electrically conductive strips 214 or a different material. These contacts 213, 215 can act as the signal input coupler 116 and the signal output coupler 118 as shown in
Optionally, at least some of sacrificial film 206 and scaffold film 208 can be removed between electrically conductive strips 214 to form electroplating gaps 224 that will allow the electroplating solution to move more freely around the helix during the electroplating process, as illustrated in
Next, sacrificial film 206 is selectively etched to release scaffold film 208, whereby strain release in scaffold film 208 causes scaffold film 208 to roll into a cylinder, bringing electrically conducting strips 214 into an end-to-end arrangement that forms an electrically conductive helix 228 (
In helix 228, each electrically conductive strip 214 (
The helix is then electroplated to increase the thickness of the electrically conductive strips from which the helix is constructed and also to fill in any gaps between the leading and trailing ends of the strips to provide a continuous helical structure. Helix 228 can be electroplated with a metal that is the same as, or different from, the metal used to form electrically conductive strips 214. Electroplating is carried out by immersing helix 228 in an electroplating solution and creating a voltage difference between plating seed 220 and a counter electrode (not shown) to induce metal ions in the electroplating solution to deposit onto the surface of helix 228.
Increasing the thickness of the helix via electroplating may provide better heat transfer and lower signal loss for the TWT amplifier and also allows for the tailoring of the signal propagating properties (e.g., operating frequencies) of the SWS, whereby smaller inner-diameter wave tubes amplify higher-frequency signals. By way of illustration only, the plating material can be deposited to thicknesses of up to 10 μm or even greater, including plating material thicknesses in the range from 30 nm to 10 μm. Using the self-assembly and electroplating processes described herein, SWSs capable of amplifying terahertz signals with frequencies in the range from 0.3 THz to 3 THz can be fabricated. Once the electroplating is completed, plating seed 220 can be removed (
Optionally, device substrate 202 can be partially or entirely removed from the TWT amplifier using, for example, a mechanical polish, wet or dry etching, or a combination thereof. Removing device substrate 202 can be advantageous because doing so reduces dielectric loading and increases interaction impedance, which increases the gain of the TWT amplifier.
The word “illustrative” is used herein to mean serving as an example, instance, or illustration. Any aspect or design described herein as “illustrative” is not necessarily to be construed as preferred or advantageous over other aspects or designs. Further, for the purposes of this disclosure and unless otherwise specified, “a” or “an” means “one or more.”
The foregoing description of illustrative embodiments of the invention has been presented for purposes of illustration and of description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and modifications and variations are possible in light of the above teachings or may be acquired from practice of the invention. The embodiments were chosen and described in order to explain the principles of the invention and as practical applications of the invention to enable one skilled in the art to utilize the invention in various embodiments and with various modifications as suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto and their equivalents.
Lagally, Max G., van der Weide, Daniel Warren, Bhat, Abhishek, Cavallo, Francesca, Dwyer, Matthew McLean
Patent | Priority | Assignee | Title |
Patent | Priority | Assignee | Title |
3916246, | |||
4571524, | Sep 26 1980 | Thomson-CSF | Electron accelerator and a millimeter-wave and submillimeter-wave generator equipped with said accelerator |
4820688, | Nov 27 1987 | UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE SECRETARY OF THE ARMY | Traveling wave tube oscillator/amplifier with superconducting RF circuit |
5112438, | Nov 29 1990 | BOEING ELECTRON DYNAMIC DEVICES, INC ; L-3 COMMUNICATIONS ELECTRON TECHNOLOGIES, INC | Photolithographic method for making helices for traveling wave tubes and other cylindrical objects |
5231330, | Oct 25 1991 | TRITON SERVICES INC | Digital helix for a traveling-wave tube and process for fabrication |
6917162, | Feb 13 2002 | Teraphysics Corporation | Traveling wave tube |
7707714, | Dec 04 2001 | MAX-PLANCK GESELLSCHAFT ZUR FORDERUNG DER WISSENSCHAFTEN E V | Method for producing a microcoil |
8847490, | Feb 21 2007 | Teraphysics Corporation | High frequency helical amplifier and oscillator |
8884519, | Feb 21 2007 | Teraphysics Corporation | High frequency helical amplifier and oscillator |
9777384, | Apr 05 2011 | The United States of America, as represented by the Secretary of the Navy; The Government of the United States of America, as represented by the Secretary of the Navy | Microfabrication of tunnels |
20030151366, | |||
20060057504, | |||
20120286657, | |||
20160099127, | |||
20170207522, | |||
20190279834, |
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